View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 37223U 26106.92528088 +.00000000 +00000-0 +16872-3 0 00004
2 37223 71.9700 179.7323 0012710 161.8768 198.2862 14.99955761 05
| Epoch (UTC): | 16 April 2026 22:12:24 |
| Eccentricity: | 0.0012710 |
| inclination: | 71.9700° |
| perigee height: | 558 km |
| apogee height: | 576 km |
| right ascension of ascending node: | 179.7323° |
| argument of perigee: | 161.8768° |
| revolutions per day: | 14.99955761 |
| mean anomaly at epoch: | 198.2862° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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